Position sensing system with an electromagnet

ABSTRACT

A position sensing system for measuring a position of a moving object includes an electromagnet configured to generate an alternating magnetic field, and a magnetic sensor configured to measure an intensity of a first magnetic field that is based on the alternating magnetic field. A controller is configured to estimate a position of the moving object based on the measured intensity of the first magnetic field.

CROSS-REFERENCE TO RELATED APPLICATIONS

This Non-Provisional patent application claims the benefit of the filingdate of U.S. Provisional Patent Application Ser. No. 62/365,829, filedJul. 22, 2016, entitled “Position Sensing System with an Electromagnet,”the entire teachings of which are incorporated herein by reference.

BACKGROUND

Potentiometers, linear variable differential transformers (LVDTs),lasers, and LED based systems may be used for position measurement. Ingeneral, the LVDT and potentiometer type of sensors require a mechanicalconnection between the moving object and the sensor. Hence, it is notpossible to use these sensors in a case where the moving object isisolated, such as a piston moving inside an engine. Making themechanical connection requires modification of the design of the system,requires assembly, and can expose the sensors to a harsh environmentwhere their performance reduces. Another limitation of these types ofsensors is that the size of the sensor increases as the range ofmeasurement increases.

Laser and LED sensors do not require mechanical connection. However,they require a clear line of sight to the moving object. Hence, theirapplication becomes limited in cases where the moving object isoptically isolated. Another requirement of the sensor is that thesurface of the moving object should reflect a certain percentage of thelaser beam. Laser and LEDs that provide sub-mm level accuracy are highlyexpensive.

Some position measurement systems that are based on magnetic fields onlyprovide a binary measurement of position (e.g., an indication of whetherthe object is to the left or the right of the sensor), and do notprovide a continuous measurement of position. Some position measurementsystems that are based on magnetic fields require installation of anextra magnet on the moving object, and an array of magnetic sensordevices is placed adjacent to the moving object. In such a system, therequired short gap (i.e., 0.5 mm to 5.5 mm) between the magnetic sensorand the moving object limits the applicability of the sensor in caseswhere a thicker isolation of the moving object is required. Anothermajor drawback of such a system is that the size of the sensor increaseswith the increase in the range of measurement of the sensor. Forexample, if it is desired to measure the position of a hydraulic pistonwhose range of motion is 500 mm, the length of the sensor should be atleast 500 mm. In some systems, the size of the magnets attached to themoving object are different based on the desired range of motion, andcan be as large as 20 mm in diameter and 7 mm in thickness, limiting theplacement of magnets in a moving piston in an engine or a hydrauliccylinder. Some of these systems also have poor linearity. The accuracyof magnetic sensors can be adversely affected by external magneticobjects coming close to the sensors.

Position sensors based on magnetic fields from permanent magnets cansuffer from error due to disturbances from ferromagnetic objects. If aferromagnetic object or other magnetic object happens to appear in thevicinity of the sensor, the position measurement of the sensor can havesignificant errors. Embodiments disclosed herein are directed to aposition measurement sensor based on an electromagnet that hassignificant robustness to disturbances from ferromagnetic objects,metallic objects and permanent magnet based disturbances.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a block diagram illustrating a position measurement systemaccording to one embodiment.

FIG. 2 is a diagram illustrating a first electromagnet-based positionsensing configuration for the position measurement system shown in FIG.1 to measure the position of a piston according to one embodiment.

FIG. 3 is a diagram illustrating a position estimation method accordingto one embodiment.

FIG. 4 is a diagram illustrating a graph of example data measuredexperimentally for the first electromagnet-based position sensingconfiguration shown in FIG. 2.

FIG. 5 is a diagram illustrating a graph of position estimates obtainedfrom the first electromagnet-based position sensing configuration shownin FIG. 2, and a comparison with the position estimates from a standarddistance measurement sensor.

FIG. 6 is a diagram illustrating a graph of the influence of aferromagnetic disturbance on the magnetic field amplitudes at theoperating frequency for the first electromagnet-based position sensingconfiguration shown in FIG. 2.

FIG. 7 is a diagram illustrating a graph that shows the robustness toferromagnetic disturbances of the first electromagnet-based positionsensing configuration shown in FIG. 2.

FIGS. 8A and 8B are diagrams illustrating a second electromagnet-basedposition sensing configuration for the position measurement system shownin FIG. 1 according to one embodiment.

FIG. 9A is a diagram illustrating a graph of the position signal sensedby the sensor for the piston position shown in FIG. 8A.

FIG. 9B is a diagram illustrating a graph of the position signal sensedby the sensor for the piston position shown in FIG. 8B.

FIG. 10A is a schematic diagram illustrating the various components thatcomprise the total magnetic reluctance between the electromagnet and themagnetic sensor in the configuration shown in FIGS. 8A and 8B accordingto one embodiment.

FIG. 10B is a diagram showing the location of the reluctance elementsshown in FIG. 10A according to one embodiment.

FIG. 11 is a diagram illustrating a graph of the RMS value of themagnetic field sensed by the sensor in an experimental implementation ofthe configuration shown in FIGS. 8A and 8B versus piston position.

FIG. 12 is a diagram illustrating a third electromagnet-based positionsensing configuration for the position measurement system shown in FIG.1 according to one embodiment.

FIG. 13 is a diagram illustrating the duty cycle for powering theexternal electromagnet shown in FIG. 12 according to one embodiment.

FIG. 14 is a diagram illustrating an example alternating current in theexternal electromagnet and a corresponding current in the internal coilfor the configuration shown in FIG. 12 according to one embodiment.

FIGS. 15A and 15B are diagrams illustrating a fourth electromagnet-basedposition sensing configuration for the position measurement system shownin FIG. 1 according to one embodiment.

FIG. 16 is a flow diagram illustrating a method of measuring a positionof a moving object according to one embodiment.

FIG. 17 is a diagram illustrating the measurement of rotational motionby the system shown in FIG. 1 according to one embodiment.

FIG. 18 is a diagram illustrating the measurement of rotational motionby the system shown in FIG. 1 according to another embodiment.

DETAILED DESCRIPTION

In the following detailed description, reference is made to theaccompanying drawings which form a part hereof, and in which is shown byway of illustration specific examples in which the disclosure may bepracticed. It is to be understood that other examples may be utilizedand structural or logical changes may be made without departing from thescope of the present disclosure. The following detailed description,therefore, is not to be taken in a limiting sense, and the scope of thepresent disclosure is defined by the appended claims. It is to beunderstood that features of the various examples described herein may becombined, in part or whole, with each other, unless specifically notedotherwise.

One embodiment is directed to a position sensing system and method forthe non-intrusive real-time measurement of the position of a movingobject, such as piston position inside a cylinder. The system includesan electromagnet to generate an alternating magnetic field, at least onemagnetic sensor for measuring an intensity of a magnetic field, and aprocessor or controller for estimating the position of the moving objectbased on the measured magnetic field.

Some embodiments may use a nonlinear model of the magnetic fieldproduced by the object as a function of position around the object. Theinherent magnetic field of a metallic object can be used to compute theposition of the object. Any ferromagnetic object has an inherentmagnetic field and this field varies as a function of the positionaround the object. If the magnetic field can be analytically obtained asa function of the position, the field intensity can be measured usingsensors and then the position of the object computed from it. Someembodiments disclosed herein may model the magnetic field around ametallic object as a function of position and use this model to estimateposition from magnetic field measurements.

The parameters in the magnetic field versus position function are uniqueto the particular object under consideration. While the functional formwill remain the same for objects of the same shape and size, theparameters in the function can vary from one object to another due tothe varying strength of magnetization. The parameters of the nonlinearmodel may be auto-calibrated or adaptively estimated by the system usingan additional redundant sensor and redundant magnetic fieldmeasurements. Some embodiments disclosed herein use an adaptiveestimation algorithm that utilizes redundant magnetic sensors to bothestimate parameters and the position.

One embodiment includes one or more of the following components: (1) anelectromagnet to generate an alternating magnetic field; (2) a set ofmagnetic field measurement sensors, longitudinally or laterallyseparated with known distances between them; (3) a nonlinear model ofthe magnetic field around the object under consideration, as a functionof the position around the object; (4) a method to calculate theposition of the object based on measurements of the magnetic field, andbased on the magnetic field as a function of position from the model;and (5) a method to adaptively estimate the parameters of the model byuse of multiple longitudinally/laterally separated redundant sensors.

FIG. 1 is a block diagram illustrating a position measurement or sensingsystem 100 according to one embodiment. System 100 includeselectromagnet 101, magnetic sensors 102, amplifier 106, analog todigital converter 108, interface 110, adaptive estimation controller114, and a model of magnetic field as a function of position 112. System100 is configured to measure the position of object 104 as the object104 moves. In some embodiments, the object 104 may include a permanentmagnet 103, and in other embodiments, the object 104 may not include thepermanent magnet 103.

In operation according to one embodiment, electromagnet 101 produces amagnetic field, and the magnetic sensors 102 continuously measure themagnetic field intensity at the location of the sensors 102. Themeasured magnetic field intensity varies as the object 104 moves. In oneembodiment, the sensors 102 include two or more magnetic field sensorsin a known configuration. Magnetic sensors 102 generate analogmeasurements based on the sensed magnetic field intensity, and outputthe analog measurements to amplifier 106, which amplifies the analogmeasurements. Amplifier 106 outputs the amplified analog measurements toanalog to digital converter 108, which converts the amplified analogmeasurements to digital measurement data. Converter 108 outputs thedigital measurement data to controller 114 via interface 110. In oneembodiment, interface 110 is a wireless interface. In anotherembodiment, interface 110 is a wired interface.

Based on the received digital measurement data and the model 112,controller 114 performs an adaptive estimation method to calculateestimated model parameters 120. Using the calculated parameters 120 inthe model 112, controller 114 continuously generates calculated positiondata 122 based on received digital measurement data. The calculatedposition data 122 provides a real-time indication of the currentposition of the object 104. In one embodiment, after calculating theestimated model parameters 120, controller 114 is also configured toperiodically update these parameters 120 during normal sensingoperations of the system 100.

In one embodiment, controller 114 comprises a computing system orcomputing device that includes at least one processor 116 and memory118. Depending on the exact configuration and type of computing device,the memory 118 may be volatile (such as RAM), non-volatile (such as ROM,flash memory, etc.), or some combination of the two. The memory 118 usedby controller 114 is an example of computer storage media (e.g.,non-transitory computer-readable storage media storingcomputer-executable instructions for performing a method). Computerstorage media used by controller 114 according to one embodimentincludes volatile and nonvolatile, removable and non-removable mediaimplemented in any suitable method or technology for storage ofinformation such as computer readable instructions, data structures,program modules or other data. Computer storage media includes, but isnot limited to, RAM, ROM, EEPROM, flash memory or other memorytechnology, CD-ROM, digital versatile disks (DVD) or other opticalstorage, magnetic cassettes, magnetic tape, magnetic disk storage orother magnetic storage devices, or any other medium that can be used tostore the desired information and that can be accessed by controller114.

One example of position sensing system 100 estimates the position of apiston inside a cylinder. In this example, the piston is the movingobject 104. Hydraulic actuators, pneumatic actuators, IC engine and freepiston engines are examples of piston-cylinder applications. Anotherexample is a rotary actuator, in which the moving object 104 is therotor, and the magnetic sensors 102 may be located on the stator (orhousing) of the actuator. Yet another example is the use of a magnet toidentify a specific location and then subsequent use of the magneticsensors 102 to determine the 3-dimensional position of that markedlocation.

When a foreign ferromagnetic object happens to come close to the sensors102, the foreign object's magnetic field may create a disturbance, whichdistorts the relationship between the location of the original object104 and its magnetic field. If the foreign ferromagnetic object remainsstationary, then the error in the original magnetic field function is aconstant at each sensor location. If the ferromagnetic object moves,then the error in the original magnetic field function is time-varying.

In order to overcome the problem of errors caused by disturbances fromferromagnetic objects, embodiments disclosed herein utilize anelectromagnet 101 as a part of the position sensing system 100. In theembodiments described below, the moving object 104 is assumed to be apiston inside a cylinder, and the system 100 uses an electromagnet-basedmethod of disturbance rejection.

In one embodiment, system 100 makes use of alternating current (AC)magnetic fields instead of time-invariant magnetic fields. In someembodiments, the electromagnet 101 is placed on the moving piston whilethe magnetic sensors 102 are placed on the cylinder. In some otherembodiments, the magnetic sensors 102 are placed on the moving pistonwhile the electromagnet 101 is placed on the cylinder.

FIG. 2 is a diagram illustrating a first electromagnet-based positionsensing configuration 200 for the position measurement system 100 shownin FIG. 1 to measure the position of a piston 204 according to oneembodiment. The electromagnet 101 (e.g., comprising a coil of wires) iswrapped around a static hydraulic cylinder 202, and the magnetic sensors102 are installed externally on the moving piston rod 206. The positionof the piston 204 may be estimated as described in further detail belowwith reference to FIG. 3.

FIG. 3 is a diagram illustrating a position estimation method 300according to one embodiment. An alternating current 302 is used to powerthe electromagnet 101. This creates an alternating magnet field 304 of aknown frequency. In one embodiment, the frequency of the magnetic field304 is chosen to be high enough to be above the bandwidth of frequenciesin which piston motion is expected. The magnetic field intensity ofmagnetic field 304 is measured by magnetic sensors 102, which produce acorresponding sensor output voltage 306.

As the piston 204 and the piston rod 206 move, the distance between thesensors 102 and the electromagnet 101 changes. The change in magneticfield amplitude that occurs with a change in distance can be modeled aswell as measured experimentally. The change in amplitude provides themechanism for distance measurement. The amplitudes of the magnetic fieldat the pre-determined frequency are measured in real-time using either afrequency demodulation chip, such as root mean square (RMS) chip 308, orby adequately fast real-time sampling, and then output as acorresponding DC output voltage 310. The distance between the sensors102 and the electromagnet 101 are then estimated using adaptiveestimation algorithms.

Robustness to ferromagnetic disturbances is obtained by the fact thatonly amplitudes of the alternating magnetic field at a particularfrequency are used in distance estimation. The presence of ferromagneticdisturbances causes a change in the magnetic field which is at a muchlower frequency than the operating electromagnet frequency. For example,a disturbance might manifest as a change in bias or DC value of themeasured magnetic fields. Since the DC value of the magnetic fields isnot utilized, the ferromagnetic disturbance does not cause any errors inthe position estimate. It should also be noted that the algorithms andelectronics used to obtain the real-time amplitudes at the operatingfrequency are fast and do not cause any significant transient errors inestimation. This method works very effectively for disturbance rejectionand provides excellent performance.

FIG. 4 is a diagram illustrating a graph of example data measuredexperimentally for the first electromagnet-based position sensingconfiguration 200 shown in FIG. 2. The vertical axis represents magneticfield amplitude (in counts) for two magnetic fields Bx1 and Bx2 measuredrespectively by two magnetic sensors 102, and the horizontal axisrepresents distance (in cm) between the sensors 102 and theelectromagnet 101. As shown in FIG. 4, the amplitude of the measuredalternating magnetic fields along the longitudinal axis varies as afunction of the distances between two magnetic sensors 102 and theelectromagnet 101 (at the operating frequency). It can be seen thatthere is a clear monotonic relationship between amplitude and distance,which enables distance estimation from the amplitude measurement.

FIG. 5 is a diagram illustrating a graph of position estimates obtainedfrom the first electromagnet-based position sensing configuration 200shown in FIG. 2, and a comparison with the position estimates from astandard distance measurement sensor. The standard distance measurementsensor that was used was a highly accurate and expensive sonar designedfor this particular distance measurement range. The vertical axisrepresents position (in cm) and the horizontal axis represents time (inseconds). It can be seen that the distance estimates (“Estimate” data)from the electromagnet based sensor compare well with the distancemeasurements (“Measured” data) from the reference sensor.

FIG. 6 is a diagram illustrating a graph of the influence of aferromagnetic disturbance on the magnetic field amplitudes at theoperating frequency for the first electromagnet-based position sensingconfiguration 200 shown in FIG. 2. The vertical axis represents magneticfield amplitude (in counts) for a magnetic field B1 measured by one ofthe magnetic sensors 102, and the horizontal axis represents time (inseconds). A large wrench was used as the ferromagnetic disturbance. Thestart of motion deviation is indicated at 602, and it is indicated at604 that the wrench introduced only small deviations from the modelcurve. While the wrench causes a significant change in magnetic fields,it does not cause a change in amplitude of the magnetic field at thehigh operating frequency of the electromagnet 101.

FIG. 7 is a diagram illustrating a graph that shows the robustness toferromagnetic disturbances of the first electromagnet-based positionsensing configuration 200 shown in FIG. 2. The vertical axis representsposition (in cm), and the horizontal axis represents time (in seconds).The graph shows distance estimates (“Estimate” data) for theelectromagnet based sensor, and the distance measurements (“Measured”data) from the reference sensor. During the period between 13 and 30seconds in the data, a large ferromagnetic wrench was waved near thesensors 102 and then placed right next to the cylinder 202. As shown inthe graph at 702, the introduction of the wrench causes barely anychanges in position estimates.

The first electromagnet-based position sensing configuration 200 shownin FIG. 2 provides several benefits, including the following: (1) Theconfiguration provides external disturbance rejection and is robust tothe introduction or presence of foreign ferromagnetic objects; and (2)the sensors 102 are completely external, and the configuration does notrequire the installation of a permanent magnet to the piston, so thesensor system can thus be easily installed or retro-fitted on existingold cylinders.

If the sensors 102 are placed on the moving object (and theelectromagnet 101 is placed on the stationary part of the cylinder 202)as shown in FIG. 2, the sensors 102 can be powered using a rechargeablebattery. One approach is to recharge the battery whenever the system isnot in use and the piston rod 206 is withdrawn fully into the cylinder202, so that the external electronics are closest to the stationary partof the cylinder 202. Automatic or inductive charging of the electronicsin this withdrawn configuration may be implemented.

FIGS. 8A and 8B are diagrams illustrating a second electromagnet-basedposition sensing configuration 800 for the position measurement system100 shown in FIG. 1 according to one embodiment. Sensing configuration800 does not require power to be supplied to the moving object. FIG. 8Ashows the piston 804 in a first position, and FIG. 8B shows the piston804 in a second position.

As shown in FIGS. 8A and 8B, the electromagnet 101 is placed around thecylinder 802, and the magnetic sensor 102 is also placed on the cylinder802 a known distance away from the electromagnet 101. A permanent ringmagnet 810 is placed on the piston 804. Electromagnet 101 generates analternating magnetic field, which is represented by alternating magneticfield lines 812.

FIG. 9A is a diagram illustrating a graph of the position signal sensedby the sensor 102 for the piston position shown in FIG. 8A. FIG. 9B is adiagram illustrating a graph of the position signal sensed by the sensor102 for the piston position shown in FIG. 8B. The vertical axisrepresents voltage, corresponding to position, and the horizontal axisrepresents time. As shown, the magnitude of the illustrated signalsvaries based on piston position.

The RMS value of the AC magnetic field read by the magnetic sensor 102for configuration 800 will not be a constant, but will depend on thelocation of the piston 804. This is because the magnetic reluctance ofthe system is influenced by the piston 804.

FIG. 10A is a schematic diagram illustrating the various components thatcomprise the total magnetic reluctance between the electromagnet 101 andthe magnetic sensor 102 in the configuration 800 shown in FIGS. 8A and8B according to one embodiment. FIG. 10B is a diagram showing thelocation of the reluctance elements shown in FIG. 10A according to oneembodiment. The permanent magnet 810 on the piston 804 and its locationcomprise the piston reluctance 1004, which is being utilized here forpiston position estimation. The reluctance of the cylinder 802 isreferred to as the core reluctance 1002. The flux through the air can beconsidered the gap reluctance 1008 plus some fringe reluctance 1010. NI1006 represents the number of turns (N) in the electromagnet 101 timesthe current (I) through the electromagnet 101.

The magnetic reluctance of the piston 804 is lower than that of air. Thetotal magnetic reluctance between the electromagnet 101 and the magneticsensor 102 depends on the magnetic reluctance of air (leakage), the corereluctance 1002 of the cylinder 802, and the magnetic reluctance of thepermanent magnet 810. Since the location of the magnet 810/piston 804influences the reluctance, the RMS value of the AC field read by thesensor 102 is influenced by the piston location, and can therefore beused to estimate piston position.

FIG. 11 is a diagram illustrating a graph of the RMS value of themagnetic field sensed by the sensor 102 in an experimentalimplementation of the configuration 800 versus piston position. Thevertical axis represents magnetic field amplitude (in counts) measuredby magnetic sensor 102, and the horizontal axis represents position (incm). The RMS value is generated by passing the signal from the sensor102 through an instrumentation amplifier, a high pass filter, and thenan RMS filter chip. There is a clear invertible relationship between RMSmagnitude and piston position.

While the configuration 800 has been shown to work and is able toestimate position, some implementations may not be as immune todisturbances as the moving electromagnet configuration 200 shown in FIG.2. This is due to the fact that the position sensing configuration heremeasures the “disturbance” caused by the piston to the alternatingfield, so the sensor may also pick up a disturbance by another object inthe same region. In an experimental implementation, the system appearedto only pick up foreign disturbances when the disturbance object wasplaced between the sensor 102 and the electromagnet 101. This can beremedied by packaging the sensor 102 with the electromagnet 101 in sucha way that no object could come between the two.

Benefits of the configuration 800 include the fact that the system doesnot require any power to be provided to a moving object. Both theelectromagnet 101 and the magnetic sensor(s) 102 are located on thestationary cylinder 802. In addition, the configuration 800 providesexternal disturbance rejection when the disturbance is outside theregion between the electromagnet 101 and the sensor 102.

FIG. 12 is a diagram illustrating a third electromagnet-based positionsensing configuration 1200 for the position measurement system 100 shownin FIG. 1 according to one embodiment. Configuration 1200 providesimmunity from disturbances, and does not require power to be supplied tothe moving object. Configuration 1200 has the potential to be completelyimmune to magnetic disturbances introduced anywhere in the neighborhoodof the piston-cylinder system. As shown in FIG. 12, externalelectromagnet 101 is located on the outside surface of cylinder 202. Asingle magnetic sensor 102 is located near the electromagnet 101 on theoutside surface of the cylinder 202. An internal inductive coil 1202 islocated on the moving piston 204. In one embodiment, the inductive coil1202 is a coil of unconnected wire that is not connected to any powersource.

FIG. 13 is a diagram illustrating the duty cycle for powering theexternal electromagnet 101 shown in FIG. 12 according to one embodiment.Waveform 1302 is the power cycle of the electromagnet 101, and waveform1304 is the period of use of the magnetic sensor signals. During the ONportion of the duty cycle waveform 1302, the external electromagnet 101is powered by an alternating current with a sufficiently high frequencyequal to the resonant frequency of the internal inductive coil 1202, andthe magnetic sensor 102 is not used. This ensures that maximum inductivecoupling occurs between the external electromagnet 101 and the internalcoil 1202. During the OFF portion of the duty cycle waveform 1302, themagnetic sensor 102 is used to measure the magnetic field of the system.Since the only electric current at this time is the current induced inthe internal coil 1202, the magnetic sensor 102 reads the magnetic fieldof the internal coil 1202. The strength of the measured magnetic fielddepends monotonically on the distance between the coil 1202/piston 204and the sensor 102.

The configuration 1200 is immune to ferromagnetic disturbances becauseit only utilizes the alternating magnetic signal at the pre-determinedresonant frequency of the internal coil 1202. All other magnetic signalsare ignored. Any other static or moving ferromagnetic objects will notcreate a magnetic field at this frequency and will therefore notinfluence the position measurement system.

FIG. 14 is a diagram illustrating an example alternating current 1402 inthe external electromagnet 101 and a corresponding current 1404 in theinternal coil 1202 for the configuration 1200 shown in FIG. 12 accordingto one embodiment. The internal coil 1202 is excited by theelectromagnet 101 during external excitation period 1406, and then themagnitude of the current 1404 gradually decreases during measurementperiod 1408 (when the electromagnet 101 is off). The measurement of themagnetic field is done when only the internal coil 1202 is active andthe external electromagnet 101 is off (i.e., during measurement period1408).

Configuration 1200 provides the ability to have an electromagnet 101 onthe moving piston 204, which results in a measurement system that isbased on an alternating magnetic field produced by the piston 204 thatis immune to ferromagnetic disturbances. In addition, the configuration1200 does not require that electrical power be connected to the movingpiston 204. Rather, the configuration 1200 transfers power inductively.It is noted that the magnetic fields created by the externalelectromagnet 101 and the internal coil 1202 will both be at the samefrequency, but it is desired to only measure the magnetic field due tothe internal coil 1202, and not the field due to the externalelectromagnet 101. This is accomplished using an on-off duty cycle asshown in FIG. 13, and measuring the magnetic field only when theexternal electromagnet 101 is turned off

FIGS. 15A and 15B are diagrams illustrating a fourth electromagnet-basedposition sensing configuration 1500 for the position measurement system100 shown in FIG. 1 according to one embodiment. FIG. 15A shows thepiston 1504 in a first position, and FIG. 15B shows the piston 1504 in asecond position (i.e., a charging position).

As shown in FIGS. 15A and 15B, the electromagnet 101 is wrapped aroundcylinder 1502, and the magnetic sensor 102 is installed externally on aproximal end of the moving piston rod 1506. In one embodiment, themagnetic sensor 102 is battery-powered with a rechargeable battery, andno wires are connected to the piston 1504. The magnetic sensor 102 andthe electromagnet 101 in the illustrated configuration are both externaldevices, and no components for position measurement are located insideof the cylinder 1502.

An inductive charging coil 1508 is positioned on a proximal end of thecylinder 1502, and an inductive receiver 1510 is positioned on or in themagnetic sensor 102. The inductive charging coil 1508 and the inductivereceiver 1510 are used to charge the battery of the magnetic sensor 102.In one embodiment, the battery of the sensor 102 is rechargedinductively each time the piston rod 1506 is fully retracted andstationary (e.g., when the piston-cylinder system is not operational, asshown in FIG. 15B). This configuration allows the magnetic sensor 102 tobe battery-powered and the battery to be automatically recharged so thatthe system can keep operating with no wired connections to thecomponents located on the piston rod 1506.

The system 100 (FIG. 1) may also be used to measure rotational motion,with the electromagnet 102 producing an alternating magnetic field, andthe magnetic sensors 102 and the controller 114 determining an angularposition. FIG. 17 is a diagram illustrating the measurement ofrotational motion by the system 100 shown in FIG. 1 according to oneembodiment. As shown in FIG. 17, the electromagnet 101 is placed on arotor 1704, and the magnetic sensors 102 are placed on a stator 1702. Inother embodiments, the electromagnet 101 is placed on the stator 1702,and the magnetic sensors 102 are placed on a rotor 1704. The controller114 (FIG. 1) determines the angular position of the rotor 1704 based onthe alternating magnetic field produced by the electromagnet 101 and themagnetic field sensed by the magnetic sensors 102.

FIG. 18 is a diagram illustrating the measurement of rotational motionby the system 100 shown in FIG. 1 according to another embodiment. Asshown in FIG. 18, the electromagnet 101 is placed on a first link of anearth moving vehicle, and the magnetic sensors 102 are placed on asecond link of the earth moving vehicle. In other embodiments, theelectromagnet 101 is placed on the second link, and the magnetic sensors102 are placed on the first link. The controller 114 (FIG. 1) determinesthe rotational angle 1802 between the first and second links based onthe alternating magnetic field produced by the electromagnet 101 and themagnetic field sensed by the magnetic sensors 102.

One embodiment is directed to a position sensing system for measuring aposition of a moving object. The system includes an electromagnetconfigured to generate an alternating magnetic field, and a magneticsensor configured to measure an intensity of a first magnetic field thatis based on the alternating magnetic field. The system includes acontroller configured to estimate a position of the moving object basedon the measured intensity of the first magnetic field. The controllermay be configured to estimate the position of the moving object basedfurther on a nonlinear model of a magnetic field produced by the movingelectromagnet as a function of position around the electromagnet.

The moving object may be a piston positioned within a cylinder. Theelectromagnet may be positioned on the piston, and the magnetic sensormay be positioned on the cylinder. The electromagnet may be positionedon the cylinder, and the magnetic sensor may be positioned on thepiston. The magnetic sensor on the piston may be powered by a battery,wherein no wires are connected to the piston.

The electromagnet and the magnetic sensor may be positioned on thecylinder. The system may further include a permanent magnet positionedon the piston. The first magnetic field may be based on both thealternating magnetic field and a magnetic field produced by thepermanent magnet.

The system may further include an inductive coil positioned on thepiston. The electromagnet may be configured to induce an alternatingcurrent in the inductive coil during on portions of an on-off duty cycleof the electromagnet. The magnetic sensor may be configured to measurethe intensity of the first magnetic field only during off portions ofthe on-off duty cycle of the electromagnet.

The electromagnet may be positioned on the cylinder and the magneticsensor may be positioned on a piston rod of the piston, wherein theelectromagnet and the magnetic sensor are external to the cylinder, andwherein no components of the position sensing system are located insideof the cylinder. The magnetic sensor on the piston rod may bebattery-powered with a rechargeable battery, and the battery may berecharged inductively each time the piston rod is fully retracted andstationary.

A frequency of the alternating magnetic field may be much higher than afrequency of motion of the moving object and may also be much higherthan a frequency of motion of any unexpected disturbances from othernearby moving magnetic or ferromagnetic objects. The controller mayinclude a high-pass or band-pass filter that extracts only an intensityof the first magnetic field at a specific known alternating frequency ofthe alternating magnetic field. The moving object may have rotationalmotion, and relative rotational motion between the electromagnet and themagnetic sensor may be used to compute a relative rotational angle ofthe moving object.

Another embodiment is directed to a method of measuring a position of amoving object. FIG. 16 is a flow diagram illustrating a method 1600 ofmeasuring a position of a moving object according to one embodiment. Inone embodiment, system 100 (FIG. 1) is configured to perform method1600. At 1602 in method 1600, an alternating magnetic field is generatedwith an electromagnet. At 1604, an intensity of a first magnetic fieldthat is based on the alternating magnetic field is measured. At 1606, aposition of the moving object is estimated based on the measuredintensity of the first magnetic field. The method 1600 may furtherinclude estimating the position of the moving object based further on anonlinear model of a magnetic field produced by the electromagnet as afunction of position around the electromagnet.

The moving object in the method 1600 may be a piston positioned within acylinder. In one example of the method, a magnetic sensor may measurethe intensity of the first magnetic field, the magnetic sensor may bepositioned on the cylinder, and the electromagnet may be positioned onthe piston. In another example of the method 1600, the magnetic sensormay be positioned on the piston, and the electromagnet may be positionedon the cylinder. In yet another example of the method 1600, theelectromagnet and the magnetic sensor may be positioned on the cylinder.

Although specific examples have been illustrated and described herein, avariety of alternate and/or equivalent implementations may besubstituted for the specific examples shown and described withoutdeparting from the scope of the present disclosure. This application isintended to cover any adaptations or variations of the specific examplesdiscussed herein. Therefore, it is intended that this disclosure belimited only by the claims and the equivalents thereof.

1. A position sensing system for measuring a position of a moving object, comprising: an electromagnet configured to generate an alternating magnetic field; a magnetic sensor configured to measure an intensity of a first magnetic field that is based on the alternating magnetic field; and a controller configured to estimate a position of the moving object based on the measured intensity of the first magnetic field.
 2. The position sensing system of claim 1, wherein the controller is configured to estimate the position of the moving object based further on a nonlinear model of a magnetic field produced by the electromagnet as a function of position around the electromagnet.
 3. The position sensing system of claim 1, wherein the moving object is a piston positioned within a cylinder.
 4. The position sensing system of claim 3, wherein the electromagnet is positioned on the piston, and the magnetic sensor is positioned on the cylinder.
 5. The position sensing system of claim 3, wherein the electromagnet is positioned on the cylinder, and the magnetic sensor is positioned on the piston.
 6. The position sensing system of claim 5, wherein the magnetic sensor on the piston is powered by a battery, and wherein no wires are connected to the piston.
 7. The position sensing system of claim 3, wherein the electromagnet and the magnetic sensor are positioned on the cylinder.
 8. The position sensing system of claim 7, and further comprising: a permanent magnet positioned on the piston.
 9. The position sensing system of claim 8, wherein the first magnetic field is based on both the alternating magnetic field and a magnetic field produced by the permanent magnet.
 10. The position sensing system of claim 7, and further comprising: an inductive coil positioned on the piston.
 11. The position sensing system of claim 10, wherein the electromagnet is configured to induce an alternating current in the inductive coil during on portions of an on-off duty cycle of the electromagnet.
 12. The position sensing system of claim 11, wherein the magnetic sensor is configured to measure the intensity of the first magnetic field only during off portions of the on-off duty cycle of the electromagnet.
 13. The position sensing system of claim 3, wherein the electromagnet is positioned on the cylinder and the magnetic sensor is positioned on a piston rod of the piston, wherein the electromagnet and the magnetic sensor are external to the cylinder, and wherein no components of the position sensing system are located inside of the cylinder.
 14. The position sensing system of claim 13, wherein the magnetic sensor on the piston rod is battery-powered with a rechargeable battery, and wherein the battery is recharged inductively each time the piston rod is fully retracted and stationary.
 15. The position sensing system of claim 1, wherein a frequency of the alternating magnetic field is much higher than a frequency of motion of the moving object and is also much higher than a frequency of motion of any unexpected disturbances from other nearby moving magnetic or ferromagnetic objects.
 16. The position sensing system of claim 1, wherein the controller includes a high-pass or band-pass filter that extracts only an intensity of the first magnetic field at a specific known alternating frequency of the alternating magnetic field.
 17. The position sensing system of claim 1, wherein the moving object has rotational motion and wherein relative rotational motion between the electromagnet and the magnetic sensor is used to compute a relative rotational angle of the moving object.
 18. A method of measuring a position of a moving object, comprising: generating an alternating magnetic field with an electromagnet; measuring an intensity of a first magnetic field that is based on the alternating magnetic field; and estimating a position of the moving object based on the measured intensity of the first magnetic field.
 19. The method of claim 15, and further comprising: estimating the position of the moving object based further on a nonlinear model of a magnetic field produced by the electromagnet as a function of position around the electromagnet.
 20. The method of claim 15, wherein the moving object is a piston positioned within a cylinder. 